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| Fuselage size (heavy load size) | 3.5m*1.5m*1.8m (L*W*H) |
| Maximum fuselage length (including main rotor) | 8m |
| Wingspan | 2.5m |
| Main rotor diameter | 5.0m |
| Take-off weight | Maximum: 500kg; Standard: 450kg |
| Mission Load - Endurance | Endurance not less than 1h for a net load of 200 kg Endurance not less than 3h at 150 kg net load Endurance not less than 5h at 120 kg net load |
| Maximum level flight speed | 140km/h |
| Cruise speed | 80-100km/h |
| Practical ceiling | 4500m |
| Standard communication uplink/downlink distance | 30-100km (optional according to actual mission requirements) |
| Wind resistance | Wind speed during takeoff and landing is not less than 12m/s (Class VI) Wind speed of not less than 16m/s (Class VII) during the airborne flight phase |
| Operating ambient temperature | -25℃～+65℃ |
| Fuselage size (heavy load size) | 3.5m*1.5m*1.8m (L*W*H) |
| Maximum fuselage length (including main rotor) | 8m |
| Wingspan | 2.5m |
| Main rotor diameter | 5.0m |
| Take-off weight | Maximum: 500kg; Standard: 450kg |
| Mission Load - Endurance | Endurance not less than 1h for a net load of 200 kg Endurance not less than 3h at 150 kg net load Endurance not less than 5h at 120 kg net load |
| Maximum level flight speed | 140km/h |
| Cruise speed | 80-100km/h |
| Practical ceiling | 4500m |
| Standard communication uplink/downlink distance | 30-100km (optional according to actual mission requirements) |
| Wind resistance | Wind speed during takeoff and landing is not less than 12m/s (Class VI) Wind speed of not less than 16m/s (Class VII) during the airborne flight phase |
| Operating ambient temperature | -25℃～+65℃ |
